This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
This specification covers pressure boundary layer control systems of turbo-jet and turbo-prop aircraft for increasing the aerodynamic lift of the wings and flaps during approach, landing, and takeoff.
This specification covers canisters for shipment and storage of lithium hydroxide (LiOH), to be used in receptacle for CO2 absorbent (see MIL-R-24159).
This specification establishes environmental criteria for designing Aerospace Ground Equipment (AGE) in support of space systems. The test levels in this specification have been elevated to compensate for absence of combined environments during test, and to allow for variations in equipment and operating conditions. Environmental requirements are summarized in Table 1.
This specification established the requirements for a 5 second duration, 4500 pound thrust (when determined at 60°F) solid propellant rocket engine hereinafter specified as 5 S-4500.
This document provides guidelines for consolidation and standardization of commercial jet transport parts, materials, and processes currently defined by two or more company or industry standards. Included in this ARP are processes for selecting and evaluating standardization opportunities as well as a procedure for initiating the development and release of global aerospace industry standards. These practices are intended to be used when two or more company standards appear to have significant overlap or in fact be technically identical. Benefits of such standardization efforts include part numbers and potentially reduced inventory levels, reduced errors, reduced qualification costs, and reduced equipment life cycle costs. This ARP is intended to be used by any two or more companies involved in the aerospace industry that wish to benefit from standardization.
This specification covers the general requirements for the design and installation of fluid anti-icing, de-greasing, and washing systems installed in military aircraft.
This specification covers the requirements for one (1) type of pocket photographic interpretation kit, containing viewing and measuring instruments, for use in the field.
This specification covers the requirements for one (1) type of pocket photographic interpretation kit, containing viewing and measuring instruments, for use in the field.
This document defines the minimum performance standards for personnel parachute assemblies to be carried in aircraft or worn by passengers, crew, or parachutists for emergency use. This document covers three types of personnel carrying parachute assemblies and the operating limitations for each:
This specification covers the design requirements and configuration of letters, numerals, and identification for aircrew station displays and control panels.